CA1248609A - Control device for controlling an engine of a turbine power system having more than one engine - Google Patents

Control device for controlling an engine of a turbine power system having more than one engine

Info

Publication number
CA1248609A
CA1248609A CA000507091A CA507091A CA1248609A CA 1248609 A CA1248609 A CA 1248609A CA 000507091 A CA000507091 A CA 000507091A CA 507091 A CA507091 A CA 507091A CA 1248609 A CA1248609 A CA 1248609A
Authority
CA
Canada
Prior art keywords
signal
engine
function
torque
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA000507091A
Other languages
English (en)
French (fr)
Inventor
Francis G. Sollman
Gerald C. Mittendorf
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Allied Corp
Original Assignee
Allied Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Allied Corp filed Critical Allied Corp
Application granted granted Critical
Publication of CA1248609A publication Critical patent/CA1248609A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/052—Torque
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/053—Explicitly mentioned power
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/13—Purpose of the control system to control two or more engines simultaneously

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Velocity Or Acceleration (AREA)
CA000507091A 1985-04-19 1986-04-18 Control device for controlling an engine of a turbine power system having more than one engine Expired CA1248609A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/725,049 US4644744A (en) 1985-04-19 1985-04-19 Control device for controlling an engine of a turbine power system having more than one engine
US725,049 1985-04-19

Publications (1)

Publication Number Publication Date
CA1248609A true CA1248609A (en) 1989-01-10

Family

ID=24912953

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000507091A Expired CA1248609A (en) 1985-04-19 1986-04-18 Control device for controlling an engine of a turbine power system having more than one engine

Country Status (4)

Country Link
US (1) US4644744A (de)
EP (1) EP0199038A1 (de)
JP (1) JPS6248933A (de)
CA (1) CA1248609A (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3830805A1 (de) * 1988-09-09 1990-03-22 Mtu Muenchen Gmbh Regelverfahren
US5095221A (en) * 1989-11-03 1992-03-10 Westinghouse Electric Corp. Gas turbine control system having partial hood control
US5315819A (en) * 1991-09-17 1994-05-31 Allied-Signal Inc. Power management system for turbine engines
US5299417A (en) * 1991-09-18 1994-04-05 Allied-Signal Inc. Apparatus for trimming autopilot commands
US5307619A (en) * 1992-09-15 1994-05-03 Westinghouse Electric Corp. Automatic NOx control for a gas turbine
US6812586B2 (en) * 2001-01-30 2004-11-02 Capstone Turbine Corporation Distributed power system
FR2858658B1 (fr) * 2003-08-06 2005-09-30 Airbus France Procede et dispositif pour l'alimentation des turboreacteurs d'un aeronef en vol automatique
US7107131B2 (en) * 2004-03-05 2006-09-12 Honeywell International, Inc. Cross-engine aircraft communication system
FR2869642B1 (fr) * 2004-04-28 2006-07-21 Eurocopter France Dispositif et procede de regulation en acceleration ou en deceleration du debit carburant d'un turbomoteur
US7509810B2 (en) * 2004-11-10 2009-03-31 Honeywell International Inc. Inter-turbine temperature display compensation method
FR2902408B1 (fr) * 2006-06-19 2008-08-08 Eurocopter France Equilibrage en puissance de deux turbomoteurs d'un aeronef
US8290683B2 (en) * 2010-02-16 2012-10-16 Telectro-Mek, Inc. Apparatus and method for reducing aircraft fuel consumption
GB2515141B (en) * 2013-03-25 2015-10-21 Honeywell Int Inc Multi-engine performance margin synchronization adaptive control system and method
US9458771B2 (en) 2013-03-25 2016-10-04 Honeywell International Inc. Multi-engine performance margin synchronization adaptive control system and method
US9221535B2 (en) 2013-09-18 2015-12-29 Honeywell International Inc. Adaptive remaining useful life balancing control system and method for multi-engine systems
US10414512B2 (en) * 2014-10-01 2019-09-17 Sikorsky Aircraft Corporation Power management between a propulsor and a coaxial rotor of a helicopter
FR3082225B1 (fr) * 2018-06-07 2020-06-05 Safran Helicopter Engines Systeme propulsif asymetrique a recuperation de chaleur
US11168621B2 (en) 2019-03-05 2021-11-09 Pratt & Whitney Canada Corp. Method and system for operating an engine in a multi-engine aircraft
US11479348B2 (en) * 2019-08-31 2022-10-25 Textron Innovations Inc. Power management systems for multi engine rotorcraft

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2942416A (en) * 1956-05-14 1960-06-28 Napier & Son Ltd Control systems for power plants having at least two power units
US3174284A (en) * 1963-02-19 1965-03-23 United Aircraft Corp Power management fuel control for plural gas turbine engines
US3200886A (en) * 1964-05-28 1965-08-17 Joseph L Magri Droop compensated fuel control system
US3307351A (en) * 1964-07-17 1967-03-07 Holley Carburetor Co Plurality of gas turbine engines torque responsive to share equally in driving a common load
US3365882A (en) * 1965-07-13 1968-01-30 Greune Christian Apparatus for the control of fuel for two or more internal combustion engines operating on the same drive shaft, especially gas turbine installations
US3403507A (en) * 1966-12-21 1968-10-01 Bendix Corp Control apparatus for equalizing an engine operating condition of a plurality of gasturbine engines
US3600888A (en) * 1970-05-12 1971-08-24 United Aircraft Corp Power management control for a multiengine installation
US3930366A (en) * 1974-07-17 1976-01-06 General Motors Corporation Helicopter power plant control
US4137721A (en) * 1977-07-22 1979-02-06 Sundstrand Corporation Control system for plural engines
US4147035A (en) * 1978-02-16 1979-04-03 Semco Instruments, Inc. Engine load sharing control system

Also Published As

Publication number Publication date
JPS6248933A (ja) 1987-03-03
US4644744A (en) 1987-02-24
EP0199038A1 (de) 1986-10-29

Similar Documents

Publication Publication Date Title
CA1248609A (en) Control device for controlling an engine of a turbine power system having more than one engine
US5023793A (en) Apparatus and method for dynamic compensation of a propeller pitch speed control governor
US4370560A (en) Compressor load control for an auxiliary power unit
US5313778A (en) Automatic turbine engine bleed valve control for enhanced fuel management
US4380893A (en) Compressor bleed air control apparatus and method
US4242864A (en) Integrated control system for a gas turbine engine
US4045955A (en) Regulating means for gas turbine plant
US4995232A (en) Running control for a gas turbine engine
JPH01310131A (ja) 燃料制御装置
US4470118A (en) Gas turbine engine fuel control
US4449360A (en) Stall detector and surge prevention feature for a gas turbine engine
CA1240380A (en) Transient derivative scheduling control system
JPH0416618B2 (de)
US6216437B1 (en) Method for regulating the power of a turbo set
JPS6018817B2 (ja) ガスタ−ビンエンジン用電子式燃料制御装置
CA2116340C (en) Helicopter engine control having yaw input anticipation
US4593523A (en) Method and apparatus for acceleration limiting a gas turbine engine
EP0394181A2 (de) Regelung der Propellerüberdrehzahl mittels digitaler Anstellwinkelsignale
US4507915A (en) Stall detector and surge prevention feature for a gas turbine engine
US4504905A (en) Digital control system including means for maintaining signals supplied thereby within limiting values
US4478038A (en) Electronic fuel control with manual training mode
EP0376875B1 (de) Rauschempfindliche signalabhängige Schaltung
US5305595A (en) Supervisory control method
US4380148A (en) Device for adjusting gas turbine engine fuel control system in accordance with engine parameter
US3588272A (en) Method and apparatus for variable pitch propellers

Legal Events

Date Code Title Description
MKEX Expiry